Boundary-layer measurements in 3.84- by 10-inch supersonic channel

Paul F. Brinichnaca-tn-2203Oct 1950

Boundary-layer measurements were made in the transonic and supersonic regions of a channel having maximum cross-sectional dimensions 3.84 by 10 inches and designed by potential-flow methods for a uniform Mach number of 2.08 in the test section.